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HARD LANDING INDICATOR FOR AN AIRCRAFT LANDING GEAR

机译:飞机起落架的硬着陆指示器

摘要

A hard landing indicator mountable to a landing gear of an aircraft isprovided. Thelanding gear has components displaceable toward each other upon the aircraftexperiencing a landing. The hard landing indicator includes a first portionsecurable toone of these components and a second portion that projects outwardly from thefirstportion and oriented toward another component of the landing gear to bepositionedwithin a path of displacement of the second component toward the firstcomponent. Thesecond portion is impacted by this component upon this component beingdisplacedduring a hard landing of the aircraft. The impact leaves a visual mark on thesecondportion of the hard landing indicator to indicate that a hard landing hasoccurred. Alanding gear equipped with and a method of installing such indicator are alsoprovided.
机译:可安装到飞机起落架的硬着陆指示器是提供。的起落架具有可在飞机上彼此相对移位的组件正在降落。硬着陆指示器包括第一部分固定于这些组件之一和第二部分从第一并朝向起落架的另一部分定向定位在第二个组件向第一个组件移动的路径内零件。的第二部分受此组件的影响流离失所在飞机硬着陆期间。撞击在机器上留下了视觉标记第二硬着陆指示器的一部分,表示硬着陆具有发生了。一种还装备了起落架及其安装方法提供。

著录项

  • 公开/公告号CA3060756A1

    专利类型

  • 公开/公告日2020-05-07

    原文格式PDF

  • 申请/专利权人 BOMBARDIER INC.;

    申请/专利号CA20193060756

  • 发明设计人 FERNELEY JOHN J. C.;

    申请日2019-10-29

  • 分类号B64D45;B64C25;

  • 国家 CA

  • 入库时间 2022-08-21 11:14:40

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